ARBITRARILY CURVED SUPPORT STRUCTURE

Abstract

The invention relates to a method for producing a support structure having a three-dimensional geometry curved in any manner, made of at least one first and one second flat material piece, wherein the geometry has curves in three directions that are orthogonal to one another, with the following steps: A. preparing the desired geometryB. approximating the desired geometryC. subdividing the geometryD. defining at least one clearance regionE. defining a plurality of connection points arranged on the at least one first and one second partF. defining chamfered edges extending between the polygonal cross-sectionsG. developing the at least one first and one second partH. cutting to length at least one first and one second flat material pieceI. chamferingJ. connecting the at least one chamfered first material piece and the at least one chamfered second material piece.

Description

The invention concerns a method of producing a carrier structure which extends in a three-dimensional geometry of any desired curvature and which comprises at least one first and one second flat piece of material, wherein the geometry has curvatures in three mutually orthogonal directions having the features of the generic term of claim 1, a carrier structure having the features of the generic term of claim 7, a computer program product and a production plant having the features of the generic term of claim 9.

Carrier structures produced in accordance with the above-described method and generic carrier structures in general, for example, can be fitted to facades of building structures and carry facade elements. This involves geometries with a preferably polygonal cross section which—depending on the respective architectural specification—must be capable of (in general of constant cross section) bending with free shaping through space. In this, especially the required twisting of the geometry about its own axis is difficult to resolve construction-wise.

The object of the invention is to provide a method in which it is possible to produce in a simple fashion carrier structures extending in a three-dimensional geometry of any desired curvature, a carrier structure which extends in a three-dimensional geometry of any desired curvature, a computer program product and a production plant.

That object is attained by a method having the features of claim 1, a carrier structure having the features of claim 7, a computer program product having the features of claim 8 and a production plant having the features of claim 9. Advantageous embodiments of the invention are defined in the dependent claims.

The invention permits the production of dimensionally accurate carrier structures in a three-dimensional geometry of any desired curvature. The geometry can be, for example, a free-form geometry or a beam geometry. A geometry which is section-wise in the form of a free-form geometry and section-wise in the form of a beam geometry is also conceivable. Connecting the at least one beveled first piece of material and the at least one beveled second piece of material along the junctions results in the desired geometry automatically and in a simple and fault-free fashion. It is possible to build carrier structures of any length. The carrier structures can be covered or planked or can carry facade elements in another fashion.

The alphabetic enumeration adopted in claim 1 of steps of the method according to the invention is not to be interpreted as a compulsory order in which the steps have to be carried out (although the specified order is, of course, possible). For example, steps B and C or D, E and F could also be carried out in any changed order.

The invention is described by means of the Figures by way of example in which:

FIG. 1 shows a depiction of an exemplary geometry

FIG. 2 shows an approximation of the geometry of FIG. 1 by a plurality of polygonal cross sections,

FIG. 3 shows a connection of the side lines of successive polygonal cross sections by loft surfaces,

FIG. 4 shows a division of the geometry into a first and a second part,

FIG. 5 shows a specification of clearance areas of adjoining loft surfaces in the area of each polygonal cross section,

FIG. 6 shows a specification of a plurality of junctions arranged at the first and second part,

FIG. 7 shows a specification of bevel edges extending between the polygonal cross sections,

FIG. 8 shows the first and second flat piece of material and the connecting pieces in the cut state,

FIG. 9 shows a beveled first piece of material, a beveled second piece of material portion and the connecting pieces,

FIG. 10 shows a clearance area of adjoining loft surfaces in the region of a piece of material which is still flat and said clearance area in a rotated and twisted state of the piece of material which is then beveled and connected to a second piece of material,

FIGS. 11a and b show an arrangement of carrier structures according to the invention in a perspective view,

FIG. 12 shows various examples of possible polygonal cross sections,

FIGS. 13 to 20 show, as alternatives to FIGS. 1 to 8, the method according to the invention with triangular polygonal cross sections instead of with quadrangular polygonal cross sections,

FIG. 21 shows an alternative way of connecting the triangular polygonal cross sections by means of connecting pieces, and

FIG. 22 shows an example of step J for the illustrative embodiment of FIGS. 1 to 9.

In order to ensure clarity of the display not all reference numbers which occur per se are shown in all Figures.

Hereinafter, by way of example a method according to the invention of producing a carrier structure 1 which extends in a three-dimensional geometry 2 of any desired curvature and which comprises at least one first and one second flat piece of material 3, 4 is described, wherein the geometry 2 has curvatures in three mutually orthogonal directions.

A first step A (FIG. 1) involves providing the desired geometry 2 in digital form. The said providing can be done in many ways known to the expert, for example in the form of CAD data, in the form of Voxel data and so forth.

A second step B involves approximating the desired geometry 2 by ascertaining a plurality of polygonal cross sections 5 along a directrix 18 of the geometry 2 (FIG. 2) and by connecting the side lines 6 of successive polygonal cross sections 5 through loft surfaces 7 (FIG. 3). Approximating the desired geometry 2 and connecting the side lines 6 of successive polygonal cross-sections 5 through loft surfaces 7 can be done manually or automated by means of standard tool commands of a CAD program. The polygonal cross sections 5 used—as illustrated—can be quadrangles, but also triangles, hexagons and so forth.

A further step C (FIG. 4) involves dividing the geometry 2 into at least one first and one second part 8, 9 which run along at least one part of the extent of the geometry 2. In relation to the polygonal cross sections 5 the division is implemented in such way that the individual side lines 6 of the polygonal cross section 5 are divided by computation, more specifically in such way as to cause a projection or an overlap between adjoining side lines 6 so that later this projection or overlap permits the cut pieces of material to be connected. In case of the quadrangular polygonal cross-section 5 illustrated this results in the individual surfaces 51 through 54 as shown. The first part 8 which is the upper part in FIG. 4 is formed by the individual surface 51. The second part 9 which is the lower part in FIG. 4 is formed by the individual surface 52. The individual surfaces 53, 54 which extend laterally in FIG. 4 later serve as connection of the first and second part 8, 9. Alternatively it would also be possible, of course, to consider the individual surfaces 53, 54 as the first or, respectively, second part 8, 9, then the individual surfaces 51 and 52 serve as the connection. Furthermore, another alternative could be to omit the individual surfaces 52 and 54 or 51 and 53 and the later connection of the first and second part 8, 9 can be effected by a displaced arrangement of those parts 8, 9 and by direct fixing to one another or by providing separate individual connecting pieces.

In the depicted preferred illustrative embodiment of a method according to the invention it is provided that dividing the geometry 2 into the at least, one first and at least one second part 8, 9 is effected in the form of shells which run along the extent of the geometry 2 and which are connected by longitudinal strips.

A further step D (FIG. 5) involves determining at least one clearance area 10 of adjoining loft surfaces 7 in the region of each, polygonal cross section 5 (in FIG. 5 the clearance areas 10, for example, extend approximately vertically in the front part). Essentially, the clearance areas 10 perform two functions. On the one hand they permit beveling of the previously flat first and second pieces of material 3, 4. On the other hand they permit twisting of the later beveled first, and second pieces of material 13, 14. The clearance areas 10 run over a corner region of the polygonal cross sections 5. The width of the clearance areas 10 can vary. The greater the local curvature, the wider the local clearance area 10 should be. The individual segments of the first and second part 8, 9 remain connected in the upper and lower parts of FIG. 5. However, this is not absolutely necessary.

A further step E (FIG. 6) involves specifying a plurality of junctions 11 arranged at the first and second parts 8, 9 along the extent of the first and one second part 8, 9 in order to later connect the at least one first and one second part 8, 9. In the example illustrated the junctions 11 are in the form of holes in order to later insert rivets, bolts, screws or the like. Alternatively the junctions 11 could also be weld points or adhesive points or weld seams or adhesive seams (line-shaped junctions 11).

A further step F (FIG. 7) involves specifying bevel edges 12 extending between the polygonal cross sections 5. That can be done by means of standard tool commands of a CAD program given manually or automated.

A further step G involves unwinding the at least one first and one second part 8, 9 which are provided with the clearance areas. 10 and junctions 11 and producing a cut contour for the at least one first and one second part 8, 9, wherein one of the curvatures located in three mutually orthogonal directions is represented in the cut contours. That can be done by means of standard tool commands of a CAD program given manually or automated.

The method steps described above can be carried out purely electronically and represent the planning part of the method according to the invention. Those method steps can be encoded in a computer program product according to the invention. The cut contours as a result of the previous method steps A to G are to be provided in electronic form or in some other suitable fashion for the procedure of cutting. Steps H to J represent the production or manufacturing part of the method according to the invention and can be carried out with a production plant according to the invention.

Step H involves cutting at least one first and one second flat piece of material 3, 4 in accordance with the cut contours in relation to the at least one first and one second part 8, 9. The cutting procedure can be carried out manually or on automated cutting machines and results in the cut first and second flat pieces of material 3, 4 shown in FIG. 8 and flat connecting pieces 15. It is to be noted that in the present disclosure the term “cutting” is used synonymously for “slicing”, “punching”, “shearing”, “lasering” and so forth.

A further step I involves beveling the cut first and second flat pieces of material 3, 4 along the bevel edges 12 to achieve a beveled first piece of material 13 and a beveled second piece of material 14. Of course, the flat connecting pieces 15 do not have to be beveled and remain flat in the illustrated example.

A further step J (see FIG. 22) involves connecting the beveled first piece of material 13 and the beveled second piece of material 14 along the junctions 11, wherein a rotating and/or twisting of mutually adjoining regions of the beveled first piece of material 13 and the beveled second piece of material 14 permitted by the clearance areas 10 is effected to represent the remaining two curvatures located in three mutually orthogonal directions and wherein the rotated and/or twisted beveled first and beveled second pieces of material portion 13, 14 are fixed by the connecting procedure The connection is preferably made manually.

In the depicted illustrative embodiment of a method according to the invention it is provided that the polygonal cross sections 5 are formed with polygons of even-numbered order (order equals four) and that at least two clearance areas 10 at opposite side lines 6 of the polygonal cross sections 5 are selected. As shown hereinafter, it is, however, also possible to use polygons with an odd-numbered order (for example, order equals three). In general it is preferably provided to use one part 53, 54 of the individual surfaces 51, 52, 53, 54 as connecting parts for the remaining individual surfaces 51, 52 in case of polygons with an even-numbered order and to directly connect (where applicable by way of extension), the individual surfaces 51, 52, 53 in the case of polygons with an odd-numbered order.

In the depicted preferred illustrative embodiment of a method according to the invention it is provided that connecting the beveled first piece of material 13 and the beveled second piece material 14 by means of the junctions 11 is effected by at least one connecting piece 15 running through at least one part of the extent of the geometry 2. This is, however, not absolutely necessary—as described above.

In the depicted preferred illustrative embodiment of a method according to the invention it is provided that the connection is made at the plurality of junctions 11 in the form of rivet connections and/or screw connections and/or weld connections and/or adhesive connections.

In the depicted preferred illustrative embodiment of a method according to the invention it is provided that the polygonal cross sections 5 are determined in such way that a surface normal 16 of each polygonal cross section 5 runs parallel to the tangent 19 of the directrix 18, that is located at a piercing point 17 of the polygonal cross section and the directrix 18.

The method described results in a carrier structure 1 according to the invention which extends in a three-dimensional curved geometry 2 and which—in the illustrative embodiment shown—comprises one first and one second beveled piece of material 13, 14, wherein the geometry 2 has curvatures in three mutually orthogonal directions (see FIG. 11).

The beveled first piece of material 13 and the beveled second piece of material 14 have clearance areas 10 produced by cuts along cut contours, wherein one of the curvatures located in three mutually orthogonal directions is represented in the cut contours (that is to say already in the flat state of the pieces of material 13, 14).

The beveled first piece of material 13 and the beveled second piece of material 14 are connected along a plurality of junctions 11 and a rotating and/or twisting process of mutually adjoining regions of the beveled first piece of material 13 and the beveled second piece of material 14, permitted by the clearance areas 10, form the remaining two of the curvatures located in three mutually orthogonal directions.

The rotated and/or twisted beveled pieces of material 13, 14 are fixed in their rotated and/or twisted form by the connecting procedure.

FIGS. 11a andb show a front view and a rear view of an arrangement 21 of carrier structures 1 according to the invention, which in the illustrated example have two longitudinal carriers which run parallel and which are bent and twisted and which are connected by transverse struts and two cover surfaces 20 fixed in a mutually spaced relationship to the longitudinal carriers. The longitudinal carriers and transverse struts are produced in accordance with the method of the invention.

FIG. 12 shows various examples for possible polygonal cross sections 5.

As an alternative to FIGS. 1 to 8, FIGS. 13 to 20 show by way of example the method according to the invention using triangular polygonal cross sections 5 instead of quadrangular polygonal cross sections 5.

FIG. 21 in turn shows an alternative way of connecting the triangular polygonal cross sections 5 (by means of connecting pieces 15).

By way of example, FIG. 22 shows step J of the method for the illustrative embodiment of FIGS. 1 to 9. The two front segments in FIG. 22 are already connected by rivets and are therefore fixed in their twisted and curved position. The remaining segments are connected consecutively.

LIST OF REFERENCES

1 carrier structure

2 geometry

3 first flat piece of material

4 second flat piece of material

5 polygonal cross section

• • 51 individual surface
  • 52 individual surface
  • 53 individual surface
  • 54 individual surface

6 side line of a polygonal cross section

7 loft surface

8 first part of the geometry

9 second part of the geometry

10 clearance area of adjoining loft surfaces

11 junction

12 bevel edge

13 beveled first piece of material

14 beveled second piece of material

15 connecting piece

16 surface normal

17 piercing point

18 directrix

19 tangent of the directrix at the piercing point

20 cover surfaces

21 arrangement

Claims

1. A method of producing a carrier structure which extends in a three-dimensional geometry of any desired curvature and which comprises at least one first and one second flat piece of material, wherein the geometry has curvatures in three mutually orthogonal directions, characterized by at least the following steps: A. providing the desired geometry in digital form,B. approximating the desired geometry by determining a plurality of polygonal cross sections along an extent of the geometry and connecting the side lines of mutually successive polygonal cross-sections by loft surfaces,C. dividing the geometry into at least one first and one second part which run along at least one part of the extent of the geometry,D. specifying at least one clearance area of adjoining loft surfaces in the area of each polygonal cross section,E. specifying a plurality of junctions arranged at the at least one first and one second part along the extent of the at least one first and one second part in order to later connect the at least one first and one second part,F. specifying bevel edges extending between the polygonal cross sections,G. unwinding the at least one first and one second part which are provided with the clearance areas and junctions and producing a cut contour in relation to the at least one first and one second part, wherein one of the curvatures located in three mutually orthogonal directions is represented in the cut contours,H. cutting at least one first and one second flat piece of material in accordance with the cut contours in relation to the at least one first and one second part,I. beveling the cut at least one first and one second flat pieces of material along the bevel edges resulting in at least one beveled first piece material and at least one beveled second piece of material, andJ. connecting the at least one beveled first piece of material and the at least one beveled second piece of material along the junctions, wherein a rotating and/or twisting procedure of mutually adjoining areas of the at least one beveled first piece of material and the at least one beveled second piece of material permitted by the clearance areas is effected to represent the remaining two of the curvatures present in three mutually orthogonal directions and wherein the rotated and/or twisted at least one beveled first and one beveled second piece of material are fixed by the connecting step.

2. A method pursuant to claim 1, wherein the polygonal cross sections are formed with polygons of even-numbered order and in step D at least two clearance areas are selected at opposite side lines of the polygonal cross sections.

3. A method pursuant to claim 1, wherein in step C the geometry is divided into the at least one first and at least one second part in the form of shells running along the extent of the geometry.

4. A method pursuant to claim 1, wherein a connection of the at least one beveled first piece of material and the at least one beveled second piece of material is effected by means of the junctions by a connecting piece running at least through at least one part of the extent of the geometry.

5. A method pursuant to claim 1, wherein in step J the connection procedure is made at the plurality of junctions in the form of rivet connections and/or screw connections and/or weld connections and/or adhesive connections.

6. A method pursuant to claim 1, wherein in step B the polygonal cross sections are determined in such way that a surface normal of each polygonal cross section runs parallel to the tangent of the directrix that is located at a piercing point of the polygonal cross section and the directrix.

7. A carrier structure which extends in a three-dimensional curved geometry and consists of at least one first and one second beveled piece of material, wherein the geometry has curvatures in three mutually orthogonal directions, whereinthe at least one beveled first piece of material and the at least one beveled second piece of material have clearance areas produced by cuts along cut contours, wherein one of the curvatures located in three mutually orthogonal directions is represented in the cut contours, andthe at least one beveled first piece of material and the at least one beveled second piece of material are connected along a plurality of junctions and a rotating and/or twisting procedure of mutually adjoining areas of the at least one beveled first piece of material and the at least one beveled second piece of material permitted by the clearance areas represent the remaining two curvatures located in three mutually orthogonal directions, andthe rotated and/or twisted at least one first beveled piece of material and at least one second beveled piece of material are fixed through the connecting procedure in their rotated and/or twisted form.

8. A computer program product including commands which when executing the program by a computer cause the same to carry out steps B to G of the method according to claim 1.

9. A production plant with a computer and production means controllable by the computer, wherein the computer is configured to actuate the production means to carry out at least one of steps H and I of the method pursuant to claim 1.